An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Charachteristics of a Tee-tail

An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Charachteristics of a Tee-tail
Title An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Charachteristics of a Tee-tail PDF eBook
Author Norman S. Land
Publisher
Pages 28
Release 1961
Genre Loads (Mechanics)
ISBN

Download An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Charachteristics of a Tee-tail Book in PDF, Epub and Kindle

An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail

An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail
Title An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail PDF eBook
Author Norman S. Land
Publisher
Pages 28
Release 1957
Genre Aerodynamics, Transonic
ISBN

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications
Title Monthly Catalog of United States Government Publications PDF eBook
Author
Publisher
Pages 1878
Release 1961
Genre Government publications
ISBN

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Technical Abstract Bulletin

Technical Abstract Bulletin
Title Technical Abstract Bulletin PDF eBook
Author Defense Documentation Center (U.S.)
Publisher
Pages 1116
Release 1961-02
Genre Technology
ISBN

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An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail

An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail
Title An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail PDF eBook
Author Norman S. Land
Publisher
Pages 1
Release 1961
Genre
ISBN

Download An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail Book in PDF, Epub and Kindle

A transonic flutter investigation was made of elastically and dynamically scaled models of the tee-tail of a patrol bomber. It was found that removal of the 15 degrees dihedral of the stabilizer used on the airplane raised the flutter boundary to higher dynamic pressures. The effect of Mach number on the flutter boundary was different for dihedral angles of 0 degrees and 15 degrees. The dynamic pressure at the flutter boundary increased approximately linearly with the torsional stiffness of the fin. Highspeed motion pictures indicated that the flutter mode consisted primarily of fin bending and fin torsion. (Author).

A Collection of Technical Papers on Structures and Materials

A Collection of Technical Papers on Structures and Materials
Title A Collection of Technical Papers on Structures and Materials PDF eBook
Author
Publisher
Pages 354
Release 1975
Genre Airplanes
ISBN

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NASA Technical Note

NASA Technical Note
Title NASA Technical Note PDF eBook
Author
Publisher
Pages 572
Release 1975
Genre
ISBN

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